Garmin GDL 84H Rotorcraft Flight Manual Supplement Download Page 1 | Manualshive

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Summary of Contents for GDL 84H

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Page 2: ...t Olathe KS 66062 USA ROTORCRAFT FLIGHT MANUAL SUPPLEMENT for STC SR02123SE GARMIN GDL 84H 88H ADS B TRANSCEIVER 190 01310 J2 Rev 1 Page 2 of 17 FAA APPROVED LOG OF REVISIONS Revision Number Date Description 1 07 29 2015 Complete Supplement ...

Page 3: ...L AURAL TRAFFIC ALERT 6 Section 3 EMERGENCY PROCEDURES 6 3 1 Emergency Procedures 6 Section 4 MALFUNCTION PROCEDURES 6 4 1 Malfunction Indications 6 Section 5 PERFORMANCE DATA 7 MANUFACTURER S DATA Section 6 WEIGHT AND BALANCE DATA 8 Section 7 PILOT CHECKLIST 8 Section 8 FUEL AND OIL DATA 8 Section 9 CHARTS AND TABLES 8 GENERAL 9 Garmin GDL 84H 88H UAT Transceiver 9 Capabilities 11 Installation Co...

Page 4: ... following system interfaces fully functional in order to be compliant with the requirements for 14 CFR 91 227 ADS B Out operations Interfaced Equipment Number Installed Number Required GPS Navigator GTN or GNS 1 or more 1 Transponder 1 or more 1 Barometric altitude source 1 or more 1 Table 2 Required Equipment 1 2 ADS B Out The GDL 84H 88H only complies with 14 CFR 91 227 for ADS B Out when all r...

Page 5: ...affic Control 1 6 Traffic Alerting Traffic alerting is an aid to visual acquisition and may not be used as the sole basis for rotorcraft maneuvering 1 7 Rotorcraft with No Heading Source Rotorcraft which do not have a heading source interfaced to the GDL 88H are subject to the following limitations The traffic page is oriented to rotorcraft TRACK which may or may not align with rotorcraft heading ...

Page 6: ...after power up if a fault was present during the previous power cycle This indicates the unit requires service but does not indicate that the unit will not comply with 91 227 The GDL 84H 88H only complies with 14 CFR 91 227 for ADS B Out when all required functions are operational as indicated when the ADS B annunciator is not illuminated 2 2 Before Takeoff GDL 84H 88H Annunciations CONSIDERED TRA...

Page 7: ... external ADS B annunciator panel if installed ADS B annunciator illuminated Transponder VERIFY ON ADS B Circuit Breaker VERIFY CLOSED When the GDL 84H detects a FAULT that does not affect compliance with requirements of 91 227 this will be annunciated to flight crew at the beginning of the next power cycle by flashing the ADS B annunciator on off for approximately 20 seconds after power up Contac...

Page 8: ...MENT for STC SR02123SE GARMIN GDL 84H 88H ADS B TRANSCEIVER 190 01310 J2 Rev 1 Page 8 of 16 MANUFACTURER S DATA Section 6 WEIGHT AND BALANCE DATA See current weight and balance data Section 7 PILOT CHECKLIST No change Section 8 FUEL AND OIL DATA No change Section 9 CHARTS AND TABLES No change ...

Page 9: ...on Legend Collective Switch Radio Altitude OR ADS B Annunciator Altitude Reporting Switch self interrogation only Bottom UAT Antenna Traffic Mute Switch Optional Altitude Source Transponder GPS Antenna ADS B Annunciator Optional Altitude Reporting On Off Switch self interrogation only Anonymous Mode Switch Optional Audio Panel TRAFFIC Annunciator Traffic Alerting Optional Traffic Aurals On Off Swi...

Page 10: ...ound station o TIS B Broadcast of secondary surveillance radar SSR derived traffic information from a ground station o FIS B Broadcast of aviation data from a ground station Reception of ADS B In data on 1090 MHz o ADS B Data directly from another transmitting aircraft o ADS R Rebroadcast of ADS B data from a ground station Provide ADS B OUT status via an ADS B annunciator lamp GDL 84H Only Provid...

Page 11: ...irements of 14 CFR 91 227 The GDL 88H meets the requirements of TSO C195a Class C1 C2 C3 C5 TIS B Services TSO C166b Class A1 and FIS B TSO C157a for ADS B In Operation and AC 20 172A for Airworthiness Approval for ADS B In Systems and Applications Installation Configuration This rotorcraft is equipped with a GDL 84H 88H system with the following interfaces features appropriate boxes will be check...

Page 12: ...AFT FLIGHT MANUAL SUPPLEMENT for STC SR02123SE GARMIN GDL 84H 88H ADS B TRANSCEIVER 190 01310 J2 Rev 1 Page 12 of 16 Anonymous Mode Not Available External Switch Controlled via display Height Above Terrain Airport Data Source Not Available Radar Altimeter GPS Navigator ...

Page 13: ...uational Awareness ENG Electronic News Gathering FIS B Flight Information Service Broadcast GDL Garmin Datalink GPS Global Positioning System GTN Garmin Touchscreen Navigator LRU Line Replaceable Unit PABI Pressure Altitude Broadcast Inhibit SBAS Satellite Based Augmentation System TCAS Traffic Collision Avoidance System In this document this term is used to refer to TCAS I TAS and TCAD systems TI...

Page 14: ...der or GTN an alternate Flight ID can be entered via those interfaces and will automatically be updated at the GDL 84H 88H Transmitted Air Ground Status The ADS B OUT message includes the air ground status of the rotorcraft Rotorcraft which do not have a Radar Altimeter OR GNS or GTN display interfaced to the GDL 84H 88H will transmit in air any time the collective is raised Rotorcraft which have ...

Page 15: ...ic alerts until becoming airborne Due to some aircraft not being required to equip for ADS B Out as well as the nature of TIS B its service volumes not all traffic will be tracked by the GDL 84H 88H This is much like an active traffic system which does not track non transponder equipped aircraft The flight crew must use see and avoid procedures to visually acquire and avoid other aircraft On Scene...

Page 16: ... system traffic alerts are provided as follows Alerts will be provided by the TCAS system for targets tracked solely via TCAS AND targets that tracked via TCAS and ADS B which are correlated Alerts will be provided by the GDL 84H 88H for targets that are tracked solely by ADS B The optional interfaced display s Pilot s Guides and supplements provide additional information regarding the functionali...

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